Oscillatory aerodynamic forces for a pitching aircraft
Keywords: Bending-torsion, Aerodynamic strip, Oscillations
AbstractChordwise aerodynamic strip derivatives for the swept back wing having bending-torsion degrees of freedom as modified by the aircraft simple harmonic pitching oscillations have been calculated.
How to Cite
Aggarwal, R. (2014). Oscillatory aerodynamic forces for a pitching aircraft. Defence Science Journal, 11(1), 12-14. https://doi.org/10.14429/dsj.11.6789
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